BLOCK DM-SL DEB
NORAD 100099
Debris
GEO
2026-028D
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GEO · NORAD 100099
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🛰️ Orbital Parameters
Perigee
34544 km
Apogee
35498 km
Inclination
0.2°
Period
1397.2 min
Mean Motion
1.03064660 rev/day
TLE Epoch
2026-09-19 15:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,021 km
Orbital Velocity11,172 km/h
Velocity3.10 km/s
Orbital Period23 hours 17 minutes
Orbits / Day1.03
Eccentricity0.0115
Semi-Major Axis41,392 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2026-02-12
Launch Site
Baikonur Cosmodrome, Kazakhstan
Int'l Designator
2026-028D
Object Type
Debris
RCS Size
Unknown
📖 About This Object
BLOCK DM-SL DEB is a tracked piece of space debris attributed to Russia (CIS), launched on 2026-02-12 from Baikonur Cosmodrome, Kazakhstan on the Elektro-L No. 5 launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Geostationary Orbit (GEO) at altitudes between 34,544 km and 35,498 km with an inclination of 0.2°. It travels at approximately 11,172 km/h (3.10 km/s), completing one full orbit every 23 hours 17 minutes — that’s roughly 1.03 orbits per day. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. As orbital debris, BLOCK DM-SL DEB poses a potential collision risk to operational satellites in nearby orbits and is continuously monitored by the U.S. Space Surveillance Network and other tracking systems.
🌍 Orbit Context
BLOCK DM-SL DEB occupies geostationary orbit at approximately 35,786 km above the equator, where its orbital period matches the Earth’s 24-hour rotation. From the ground, it appears to hover over a fixed point — ideal for broadcast television, weather monitoring and wideband communications. Within ±50 km of BLOCK DM-SL DEB’s average altitude, there are currently 0 active payloads and 13 tracked debris or rocket body fragments. Russia (CIS) operates approximately 1,537 active satellites in total.
🔗 Tracked Space Debris
This is a tracked piece of orbital debris — a fragment from a collision, explosion, or separation event that no longer serves any useful purpose. Space surveillance networks catalogue objects larger than approximately 10 cm in LEO. Even small debris can be catastrophic at orbital velocities (7–8 km/s in LEO), carrying kinetic energy comparable to a hand grenade per centimetre-sized fragment. The growing debris population is one of the most pressing challenges for long-term space sustainability.
❓ Frequently Asked Questions
BLOCK DM-SL DEB orbits at approximately 35,021 km altitude, where the orbital period matches the Earth’s 24-hour rotation. This means it stays above the same point on the equator at all times. Its actual speed is still 11,172 km/h — it just keeps pace with the ground below. Learn more about geostationary orbits.
BLOCK DM-SL DEB (NORAD ID 100099) is a piece of tracked orbital debris attributed to Russia (CIS). It was likely created by a fragmentation event, collision, or mission-related separation. Even small debris objects at orbital velocities carry enormous kinetic energy, so they are tracked by the U.S. Space Surveillance Network to enable collision avoidance for operational satellites.
BLOCK DM-SL DEB was launched on 2026-02-12 from Baikonur Cosmodrome, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. View the full satellite launch log.
Yes — Orbital Radar tracks BLOCK DM-SL DEB (NORAD ID 100099) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. Open the live tracker to see its current position, altitude, speed and orbital path updated in real time. You can also browse the satellite directory to find other tracked objects.
BLOCK DM-SL DEB travels at approximately 11,172 km/h (6,942 mph) — roughly 3.10 km/s. Despite this high speed, it appears stationary from the ground because it matches the Earth’s rotation. Geostationary satellites are actually slower than LEO satellites because orbital velocity decreases with altitude.
All tracked debris poses a potential collision risk to operational satellites. At orbital velocities, even a small object carries enormous kinetic energy — a 1 cm fragment at 3.10 km/s has the energy equivalent of a hand grenade. Space agencies perform routine conjunction assessments and may manoeuvre operational satellites to avoid tracked objects like BLOCK DM-SL DEB. Read more about debris statistics and the Kessler syndrome.